... I)! ne-at (n = 1,2,3,. . .) sin wt cos wt sinh wt cosh at 1 - (1 - eCat) a 1 (e-at - e-bt) b-a 1 - (be-bt - ae-at) b - a 1 (be-at - ae-bt I - I +- ab '[ ... (1 - e-"' - a2 1 7 (at - 1 + e *) a e-"' sin wt ePar cos wt e-cmntsinwndmt - 1 e-Cwnt sin (w, dm t - @)...
Ngày tải lên: 12/08/2014, 02:20
Ogata - Modern Control Engineering Part 2 pps
... - Pn-1~ = in-1 - Pn-IU where Po, PI, P2, . . . , Pn are determined from Po = bo P1 = bl - a1Po PZ = b2 - alp1 - a2Po P3 = b3 - alp2 - a2P1 - Pn = bn - ... state vari- ables.) With the present choice of state variables, we obtain x1 = X2 + plu x2 = X3 + P211 ( 3-4 0) xn-I = XI1 + Pt 1-1 ~ - in -...
Ngày tải lên: 12/08/2014, 02:20
Adaptive Control 2011 Part 14 potx
... via an adaptive control technique to guarantee the stability margin. Finally, we 0 2 4 6 8 10 -1 .4 -1 .2 -1 -0 .8 -0 .6 -0 .4 -0 .2 0 0.2 Time [ sec ] x 1 [cm] 0 2 4 6 8 10 -2 0 -1 5 -1 0 -5 0 5 10 15 20 25 Time [ sec ] x 2 [ cm / s ] 0 ... Automatic Control, 43, 3, 33 6-3 50. Li, Z. & Krstić, M. (1997). Optimal design of adaptive tracking control...
Ngày tải lên: 21/06/2014, 19:20